00-340-9313
Structural Aircraft Panel
Used on kc-135 stratolifter aircraft.
00-340-9314
Structural Aircraft Panel
Used on kc-135 stratolifter aircraft.
00-340-9315
Structural Aircraft Panel
Used on kc-135 stratolifter aircraft.
00-340-9349
Structural Aircraft Panel
Used on kc-135 stratolifter aircraft.
00-340-9393
Aircraft Door
00-340-9412
Structural Aircraft Plate
Used on acft model kc-135.
00-340-9437
Structural Aircraft Plate
00-340-9477
Access Aircraft Cover
00-340-9523
Structural Aircraft Plate
Used on kc=135 tanker airplane. 2.500" overall length 2.500" overall width 0.500" material thickness 1.204 in dia center hole, 4 mounting holes 0.223 in. dia
00-340-9938
Exhaust Pipe Flange
T-33a
00-340-9953
Structural Component Air Fitting
1.680" overall length u/a: swing joint ftg; matl:steel
00-340-9984
Structural Aircraft Panel
00-340-9991
Aircraft Door
Used on F-104.
00-341-0032
Structural Component Air Fitting
U/a: ammunition fitting
00-341-0036
Aircraft Skin
00-341-0037
Aircraft Skin
00-341-0038
Aircraft Skin
00-341-0040
Structural Component Air Bracket
00-341-0059
Structural Component Air Support
00-341-0084
Structural Component Air Support
2.559" overall length matl: steel, LS4802; 0.375in min 0.383in max dia hole thru base two places
00-341-0093
Aircraft Latch Assembly
Latch assembly, forward
00-341-0115
Aircraft Fairing
29.500" overall length 19.500" overall width
00-341-0137
Structural Component Air Support
00-341-0138
Structural Component Air Support
00-341-0147
Structural Aircraft Plate
Aluminum alloy 2024-T4 per qq-a-250/5, 1.100 in. lg, 0.750 in. w, 0.100 in. thk, 1 ea 0.198 in. min, 0.204 in. max center hole, 250 microinch finish, 1 surface serrated
00-341-0150
Structural Component Air Support
00-341-0729
Structural Component Air Support
00-341-0730
Structural Component Air Support
00-341-5858
Structural Component Air Bracket
00-341-6140
Access Aircraft Cover
0.218" hole diameter
00-341-6184
Access Aircraft Cover
Used on kc-135 aircraft. 0.218" hole diameter anodize surface treated
00-341-6285
Structural Component Air Support
3.600" overall length 2.500" overall width
00-341-6324
Structural Component Air Support
00-341-6342
Structural Component Air Support
2.559" overall length matl:steel, LS4802; 0.376in min, 0.383in max dia hole thru base 2 places
00-341-6352
Structural Component Air Bracket
1.750" material thickness matl:steel 8630
00-341-6353
Aircraft Latch Assembly
00-341-8910
Structural Component Air Support
Aluminum alloy
00-341-8912
Aircraft Hinge
00-341-8914
Aircraft Hinge
00-341-8945
Structural Component Air Bracket
U/a:cowl flap valve bracket; matl aluminum
00-342-1440
Structural Component Air Support
Used on acft model b-52. aluminum alloy, qq-a-225/6, 3.370 in. lg, 1.470 in. w, 1.370 in. h, 0.188 in. min, 0.189 in. max dia hole 1 in line 2 places
00-342-1441
Structural Component Air Support
Used on acft model b-52. aluminum alloy, qq-a-225/6, 3.370 in. lg, 1.470 in. w, 1.370 in. h, 0.188 in. min, 0.189 in. max dia hole 1 in line 2 places
00-342-1443
Structural Component Air Support
Used on acft model b-52. aluminum alloy, qq-a-225/6, 3.370 in. lg, 1.220 in. w, 1.370 in. h, 0.188 in. min, 0.189 in. max dia hole 1 in line 2 places
00-342-1471
Structural Aircraft Plate
00-342-1544
Structural Aircraft Panel
00-342-1606
Aircraft Former
Used on T-33.
00-342-1620
Structural Component Air Fitting
